کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
5003045 | 1368462 | 2016 | 6 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
LPV Control and Singularity Avoidance of a Spacecraft with DGCMGs
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
سایر رشته های مهندسی
مکانیک محاسباتی
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چکیده انگلیسی
In this paper, we analyze the dynamics of a spacecraft with Multiple Double-Gimbal Control Moment Gyros (DGCMGs). After local linearization of this nonlinear dynamics, we develop an easy-to-use Linear Parameter-Varying (LPV) model, in which we deal with 3-axis attitude control of a spacecraft equipped with two parallel DGCMGs. Then, we propose a singularity robustness (SR) steering law together with a sigmoid function as a singularity robust parameter. Although it is hard to consider overall stability and control performance of attitude control at the same time with conventional Lyapunov function-based controllers, this paper attains both of approximate stability and control performance via LPV control theory, while using redefining the control input of the generalized plant. Through a numerical example, usefulness of the proposed method is demonstrated.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: IFAC-PapersOnLine - Volume 49, Issue 17, 2016, Pages 152-157
Journal: IFAC-PapersOnLine - Volume 49, Issue 17, 2016, Pages 152-157
نویسندگان
Takahiro Sasaki, Takashi Shimomura, Sayaka Kanata,